CH373922A - Ringspaltdüse für Rückstosstriebwerke - Google Patents
Ringspaltdüse für RückstosstriebwerkeInfo
- Publication number
- CH373922A CH373922A CH105061A CH105061A CH373922A CH 373922 A CH373922 A CH 373922A CH 105061 A CH105061 A CH 105061A CH 105061 A CH105061 A CH 105061A CH 373922 A CH373922 A CH 373922A
- Authority
- CH
- Switzerland
- Prior art keywords
- annular gap
- gap nozzle
- recoil
- engines
- recoil engines
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Testing Of Engines (AREA)
- Fuel-Injection Apparatus (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB56534A DE1151409B (de) | 1960-02-05 | 1960-02-05 | Ringspaltduese fuer Raketentriebwerke |
Publications (1)
Publication Number | Publication Date |
---|---|
CH373922A true CH373922A (de) | 1963-12-15 |
Family
ID=6971363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH105061A CH373922A (de) | 1960-02-05 | 1961-01-30 | Ringspaltdüse für Rückstosstriebwerke |
Country Status (4)
Country | Link |
---|---|
US (1) | US3210929A (de) |
CH (1) | CH373922A (de) |
DE (1) | DE1151409B (de) |
GB (1) | GB965561A (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0028477A1 (de) * | 1979-10-31 | 1981-05-13 | Wallop Industries Ltd | Raketenmotor |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3358933A (en) * | 1962-09-14 | 1967-12-19 | Aerojet General Co | Rocket nozzle with automatically adjustable auxiliary nozzle portion |
DE1223198B (de) * | 1963-10-02 | 1966-08-18 | Dynamit Nobel Ag | Rakete mit Ringduese |
US3332235A (en) * | 1965-12-16 | 1967-07-25 | Thiokol Chemical Corp | Rotary device |
US3831396A (en) * | 1971-08-19 | 1974-08-27 | Aeronautical Res Ass Of Prince | Self-regulating thermal protection system for heated surfaces |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR502560A (fr) * | 1916-08-21 | 1920-05-19 | Procedes Westinghouse Leblanc | Torpille aérienne |
BE425483A (de) * | 1937-01-04 | |||
DE729133C (de) * | 1939-05-12 | 1942-12-10 | Bohdan Pantoflicek | Verschluss von Treibfuellungen von Minen, Geschossen, Granaten u. aehnl. |
US2406560A (en) * | 1943-12-30 | 1946-08-27 | Winslow B Pope | Rocket motor |
US2563270A (en) * | 1944-02-14 | 1951-08-07 | Lockheed Aircraft Corp | Gas reaction power plant with a variable area nozzle |
US2633702A (en) * | 1946-02-28 | 1953-04-07 | Clarence N Hickman | Multiple nozzle rocket |
US2468820A (en) * | 1947-02-01 | 1949-05-03 | Daniel And Florence Guggenheim | Means for cooling projected devices |
US2544422A (en) * | 1948-05-15 | 1951-03-06 | Daniel And Florence Guggenheim | Cooling means for a combustion chamber and nozzle in which solid fuel is burned |
US2648191A (en) * | 1951-08-20 | 1953-08-11 | Ca Nat Research Council | Heat power reactor |
US2780914A (en) * | 1951-12-20 | 1957-02-12 | Gen Electric | Ambient pressure responsive control for fuel oxidizer and nozzle exhaust area of reaction motors |
US2743576A (en) * | 1952-02-28 | 1956-05-01 | Crockett Sydney Robert | Propellant impelled turbine |
US2870599A (en) * | 1952-12-06 | 1959-01-27 | Theodore M Long | Temperature responsive rocket nozzle |
GB792910A (en) * | 1953-06-19 | 1958-04-02 | Havilland Engine Co Ltd | Reaction turbines |
US2909032A (en) * | 1956-10-24 | 1959-10-20 | Thiokol Chemical Corp | Temperature compensating nozzle |
US3026806A (en) * | 1957-03-22 | 1962-03-27 | Russell Mfg Co | Ballistic missile nose cone |
-
1960
- 1960-02-05 DE DEB56534A patent/DE1151409B/de active Pending
-
1961
- 1961-01-30 CH CH105061A patent/CH373922A/de unknown
- 1961-01-31 US US86190A patent/US3210929A/en not_active Expired - Lifetime
- 1961-02-02 GB GB3981/61A patent/GB965561A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0028477A1 (de) * | 1979-10-31 | 1981-05-13 | Wallop Industries Ltd | Raketenmotor |
Also Published As
Publication number | Publication date |
---|---|
GB965561A (en) | 1964-07-29 |
US3210929A (en) | 1965-10-12 |
DE1151409B (de) | 1963-07-11 |
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